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You searched for: publisher:"Washington, D.C. : NACA"
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[texts]Formation of a vortex at the edge of a plate - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874042&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 71
[texts]Nonstationary gas flow in thin pipes of variable cross section - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804176&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Difference equations; Gas flow
Downloads: 155
[texts]Comparison of measured and predicted indicated angles of attack near the fuselages of a triangular-wing wind-tunnel model and a swept-wing fighter airplane in flight - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808552&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings, Triangular; Fighter planes--Wings--Testing; Aerodynamics--Research
Downloads: 71
[texts]Experimental determination of local and mean coefficients of heat transfer for turbulent flow in pipes - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778687&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Heat--Transmission
Downloads: 173
[texts]Resistance of cascade of airfoils in gas stream at subsonic velocity - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779974&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamics; Laminar boundary layer
Downloads: 91
[texts]On the contribution of turbulent boundary layers to the noise inside a fuselage - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874415&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulent boundary layer--Research; Airplanes--Fuselage
Downloads: 63
[texts]Experimental investigation of the effects of viscosity on the drag of bodies of revolution at a Mach number of 1.5 - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810752&ix=nu&I=0&V=D&pm=1
Keywords: Body of revolution; Drag (Aerodynamics; Aerodynamics--Research
Downloads: 46
[texts]On the spectrum of natural oscillations of two-dimensional laminar flows - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874406&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar flow--Research
Downloads: 140
[texts]On the determination of certain basic types of supersonic flow fields - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807561&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics, Supersonic; Aeronautics--Research
Downloads: 132
[texts]Theories of turbulence - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807732&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence; Aerodynamics--Research
Downloads: 142
[texts]Systematic investigations of the influence of the shape of the profile upon the position of the transition point - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875302&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Boundary layer--Research
Downloads: 138
[texts]Apparatus for measurements of time and space correlation - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807826&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence--Research; Aerodynamics--Research
Downloads: 73
[texts]Laminar flow about a rotating body of revolution in an axial airstream - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874362&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer; Rotational motion (Rigid dynamics
Downloads: 92
[texts]Concerning the flow about ring-shaped cowlings.: Part VIII, further measurements on annular profiles - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779491&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Radiators--Thermodynamics
Downloads: 60
[texts]Measurement of heat-transfer and friction coefficients for flow of air in noncircular ducts at high surface temperatures - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808103&ix=nu&I=0&V=D&pm=1
Keywords: Skin friction (Aerodynamics; Nusselt number; Aerodynamics--Research
Downloads: 196
[texts]Some experiences regarding the nonlinearity of hot wires - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003760215&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Heat--Transmission
Downloads: 59
[texts]Flow of gases in narrow channels - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779980&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 89
[texts]Concerning the flow about ring-shaped cowlings.: Part XII, two new classes of circular cowls - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003769345&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Radiators--Thermodynamics
Downloads: 54
[texts]Plane problem of the flapping wing - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780265&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Wings--Testing
Downloads: 82
[texts]Review of the physical and thermodynamic properties of boric oxide - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853251&ix=nu&I=0&V=D&pm=1
Keywords: Thermodynamics--Research; Aerodynamics--Research
Downloads: 65
[texts]Heat transfer and pressure measurement on a 5-inch hemispherical concave nose at a Mach number of 2.0 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834297&ix=nu&I=0&V=D&pm=1
Keywords: Skin friction (Aerodynamics; Noses (Aircraft; Heat--Transmission
Downloads: 60
[texts]Flat plate cascades at supersonic speed - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807842&ix=nu&I=0&V=D&pm=1
Keywords: Cascades (Fluid dynamics; Aerodynamics--Research
Downloads: 69
[texts]General solutions of optimum problems in nonstationary flight - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807493&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Flight testing; Aerodynamics--Research
Downloads: 72
[texts]Some measurements of time and space correlation in wind tunnel - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807829&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence--Research; Aerodynamics--Research
Downloads: 98
[texts]Displacement effect of the laminar boundary layer and the pressure drag - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779843&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Laminar boundary layer
Downloads: 164
[texts]experimental investigation at a Mach number of 2.01 of the effects of body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853000&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings, Swept-back; Aerodynamics--Research
Downloads: 66
[texts]Investigations on reductions of friction on wings, in particular by means of boundary layer suction - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875288&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Boundary layer--Research; Airplanes--Wings--Testing
Downloads: 106
[texts]On the instability of methods for the integration of ordinary differential equations - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875150&ix=nu&I=0&V=D&pm=1
Keywords: Numerical integration; Differential equations
Downloads: 72
[texts]On the gas dynamics of a rotating impeller - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807542&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 81
[texts]Kinetic treatment of the nucleation in supersaturated vapors - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807766&ix=nu&I=0&V=D&pm=1
Keywords: Atmospheric nucleation; Aerodynamics--Research
Downloads: 82
[texts]Cooling characteristics of a transpiration-cooled afterburner with a porous wall of brazed and rolled wire cloth - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808495&ix=nu&I=0&V=D&pm=1
Keywords: Afterburners--Research; Aerodynamics--Research
Downloads: 67
[texts]Drag reduction by suction of the boundary layer separated behind shock wave formation at high mach numbers - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003760239&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Boundary layer
Downloads: 89
[texts]On the problem of gas flow over an infinite cascade using Chaplygin's approximation - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874033&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 72
[texts]Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 2.04 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809150&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics--Research; Drag (Aerodynamics
Downloads: 177
[texts]Concerning the flow about ring-shaped cowlings.: Part XIII, the influence of a projecting hub - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003769590&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Jet engines--Air intakes
Downloads: 87
[texts]Experimental heat-transfer and friction coefficients for air flowing through stacks of parallel flat plates - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808501&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamic heating; Aerodynamics--Research
Downloads: 77
[texts]Heat transmission in the boundary layer - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003759949&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulent boundary layer
Downloads: 103
[texts]Approximate method for estimating the incompressible laminar boundary-layer characteristics on a flat plate in slipping flow - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810747&ix=nu&I=0&V=D&pm=1
Keywords: Laminar boundary layer; Aerodynamics--Research
Downloads: 72
[texts]Autogenous welding in airplane construction - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874350&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Design and construction; Oxyacetylene welding and cutting
Downloads: 229
[texts]Langley full-scale-tunnel tests of the custer channel wing airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808518&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 80
[texts]Flat wing with sharp edges in a supersonic stream - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874043&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 160
[texts]On the design of airfoils in which the transition of the boundary layer is delayed - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778659&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar flow; Aerofoils
Downloads: 126
[texts]Finite span wings in compressible flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807553&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings--Testing; Aerodynamics--Research
Downloads: 69
[texts]Theoretical determination of low-drag supercavitating hydrofoils and their two-dimensional characteristics at zero cavitation number - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834476&ix=nu&I=0&V=D&pm=1
Keywords: Hydrofoils; Aerodynamics--Research
Downloads: 76
[texts]Contributions to the theory of the spreading of a free jet issuing from a nozzle - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779926&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Jet nozzles
Downloads: 58
[texts]Flow past a straight- and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808476&ix=nu&I=0&V=D&pm=1
Keywords: Body of revolution; Aerodynamics--Research
Downloads: 51
[texts]Infinitesimal conical supersonic flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780782&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Differential equations
Downloads: 143
[texts]On the recording of turbulent longitudinal and transverse fluctuations - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779925&ix=nu&I=0&V=D&pm=1
Keywords: Buffeting (Aerodynamics; Turbulent boundary layer
Downloads: 60
[texts]Gas flow with straight transition line - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003871226&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 163
[texts]Theoretical and experimental investigation of arbitrary aspect ratio, supercavitating hydrofoils operating near the free water surface - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834456&ix=nu&I=0&V=D&pm=1
Keywords: Hydrofoils; Aerodynamics--Research
Downloads: 107
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